• ICROS
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• v.22 no.2
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• pp.29-33
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• 2016

본 기술 특집호에서는 최근메 강인제어 분야에서 많이 주목받고 있는 사전규정 오차 구속제어기법들메 대해 기본적인 개념과 각 구속제어 기법들이 특징들을 소개한다. 기존의 제어기법들은 안정도 및 일정한 출력성능은 보장하지만 선정된 제어기 게인 값에 따라 추종성능이 민감하게 변하며 안전을 위한 제약이 없는데 반해 이러한 구속제어는 최소한의 게인 선정으로 오버슈트, 정상오차 등에 대해 사전에 규정한 성능범위를 만족하도록 강제로 구속시켜 출력성능 및 안전성이 동시에 보장되도록 한다. 이러한 구속제어는 오버슈트에 크게 영향을 받는 정밀기기 위치제어, 힘 제어에서 안전성을 확보해주며 외란이나 시스템 불확실성에 매우 강인한 특성을 갖는다. 가장 먼저 연구된 구속제어는 funnel 제어로서 시스템의 동적 모델을 포함하지 않는 비모델 기준 제어기법이다. 추종오차의 초기값이 오차에 대한 사전 구속함수로 구성된 funnel (깔데기) 안에 있으면 항상 사전메 규정된 오차범위 내에 머물도록 funnel 제어기가 작동하며 PD 제어와 구조가 유사하다. 다음으로 tanh 함수와 추종오차 변환을 결합한 방법으로서 전통적인 순환적 (recursive) 제어방법인 backstepping 제어와 결합하는 방법이다. 최종적므로 좀더 단순한 오차변환을 통해 오차에 대한 switching을 이용한 기법은 제어기 구조를 단순하게 만들고 기존의 제어기와 편리하게 결합할 수 있다. 이러한 구속제어 기법들은 또한 미지의 시스템에 특성에 대해 관측기나 지능제어를 이용한 근사함수를 요구하지 않는다. 본 특집호에서는 최근까지 연구된 구속제어에 대한 간단한 이론과 적용 결과들을 제시하기로 한다.

• Journal of the korean Society of Automotive Engineers
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• v.23 no.6
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• pp.12-20
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• 2001

• Proceedings of the Korea Institutes of Information Security and Cryptology Conference
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• 1992.11a
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• pp.153-164
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• 1992

EDI 체계가 정착되기 위해서는 EDI 메세지가 법적 구속력이 있는 상용 전자문서이므로 전자문서 전달에 관련된 사람이나 장비가 기존의 상거래에서 유지되는 안전성보다 더욱 철저하게 전자문서를 관리하여야 하며, 안전성 문제의 해결책이 없이는 EDI화의 진척은 한계에 부딪치게 된다. 본 논문에서는 EDI 통신에 관련된 분야 중에서 메세징 시스템 분야의 안전성을 위해 X. 435에서 정의하고 있는 안전성 서비스를 구현하기 위한 방안에 대해서 연구하였다.

• Journal of Advanced Navigation Technology
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• v.26 no.2
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• pp.47-53
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• 2022

With the recent development of defense technology, various aircraft armaments/equipments are being developed. Among them, cruise guided weapons(missile) for launching aircraft can be installed on aircraft aftersecuring reliability and safety through varioustests. In order to avoid collision with aircraft, missile separated from aircraft must release restraint of wing at the specified time, control wing in the specified direction. In order to confirm this, a test system that can control MIL-STD-1760 according to safety separation procedure and verify release performance is required. test system needs a function to check circuit for release of restraints and a function to check driving performance by controlling MIL-STD-1760. In addition, test system should be simulate environment separated from aircraft. This paper presented a testsystemthat can verify circuit and driving performance mounted on missile according to the safety separation procedure, and it was confirmed that it was normally separated from aircraft through flight tests.

• Journal of Aerospace System Engineering
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• v.12 no.2
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• pp.37-45
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• 2018

A two-axis gimbal-type antenna for a Compact Advanced Satellite (CAS) is used to efficiently transmit high resolution image data to a ground station. In this study, we designed the structure of a two-axis gimbal-type antenna while applying a launch lock device to secure its structural safety under a launch environment. To validate the effectiveness of the structural design, a structural analysis of the antenna was performed. First, a modal analysis was performed to investigate the dynamic responses of the antenna with and without the mechanical constraints of the launch lock device. In addition, a quasi-static analysis was performed to confirm the structural safety of the antenna structure and bolt I/Fs between the antenna base and the satellite. The suitable range of constraint force on the launch lock device was also determined to ensure the structural safety and mechanical gapping of the ball & socket interfaces, which places multi-constraints on the azimuth and elevation stage of the antenna.

• Journal of Aerospace System Engineering
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• v.16 no.6
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• pp.123-128
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• 2022

This paper proposes a non-explosive separation device for the deployable SAR antenna. This device utilises a Ni-Cr wire to restrain the antenna's belt mechanism, and joule-heating is used to minimise the impact of deployment. After the Ni-Cr wire has been cut, the device is deployed through the preload of the belt mechanism. Considering the design load(99g) and preload conditions, FEM analysis for AL7050 and Ti was performed. This analysis revealed that the amount of deformation for AL7050 was 0.256 mm with a margin of +0.09. In addition, by performing orbital thermal analysis, the temperature distribution for AL7050 in the worst cold case is confirmed as -50 to +2℃ and -10 to +90℃ in the worst hot case. This analysis confirmed that the separation device would remain stable even in the worst environment.

• Proceedings of the ESK Conference
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• 1995.10a
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• pp.91-100
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• 1995

자동차의 안전도는 전통적으로 정면 충돌시 승객의 보호 정도를 가지고 비 교 된다. 그러나 근래에 와서는 다양한 사고에 의한 승객의 피해를 볼 때 정면 과 더불어 측면 충돌시의 피해를 무시할 수 없는 상태에 이르렀다. sled tests 등을 통해서 정면 뿐만 아니라 측면 충돌의 영향도 파악하고 있으나 정면 충돌보다 측면 충돌에 대해 승개 보호 장치의 개발이 미흡한 것이 현실이다. 본 연구에서는 현실적으로 보다 효과적인 occupant (운전자 및 승객) restraint system을 computer 모의 실험을 통해서 제안하고자 하였다. 기존의 안전시스템인 lap/shoulder belt system과 Air cushion에 의한 실험은 다각도로 연구되었다. 그러나 측면 충돌에서 Air Bag에 의한 충돌 감소 영향은 정면 충돌에 비해 적어지게 되어 상체 측면 보호 장치가 필요하게 된다. 본 연구에서는 운전자의 lap/shoulder belt system과 Air Bag에 의해 구속되는 dummy를 가지고 다양한 측면 충돌 각도 (0 .deg. , 15 .deg. , 30 .deg. , 45 .deg. , 70 .deg. )에서 실험이 수행되었다. 또한 각 충돌각에 대해 기존 Restraint System에 상체 측면 보호 장치(seat wing)를 포함하여 실험을 수행 하였다. 이에 대한 각각의 영향, 그리고 승객 손상도 분석 및 평가를 통하여 보안된 측면 충돌 보호 restraint system의 필요성과 그 효과를 제시하고자 한다. 실험결과 에 의하면 정면보다 측면에서 충돌하였을 경우 보조 구속 시스템인 seat wing으로 인 해 측면보호는 물론 occupant는 정면으로 나가게 개선되어 구속 시스템으로써의 이점이 확대되고 shoulder blet 또는 dummy의 감속을 통제하는 Air Bag의 잠재적인 이점이 더욱 확대되었음을 보여주고 있다. 그러나 design 단계에서 편안함, 안락감 등의 문제들과, 다른 실용적인 면에 대한 계속적인 연구가 필요하다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.26 no.2
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• pp.165-171
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• 2013

Due to the difficulty in considering dynamic load in the view point of a computer resource and computing time, it is common that external load is assumed as ideal static loads. However, structural analysis under static load cannot guarantee the safety of design of the structures under dynamic loadings. Recently, the systematic method to construct equivalent static load from the given dynamic load has been proposed. Previous study has calculated equivalent static load through the optimization procedure under displacement constraints. However, previously reported works to distribute equivalent static load were based on ad-hoc methods. Improper selection of equivalent static loading positions may results in unreliable prediction of structural design. The present study proposes the selection method of the proper locations of equivalent static loads to dynamically applied loads when we consider transient dynamic structural problems. Moreover, it is appropriate to take into account the stress constraint as well as displacement constraint condition for the safety design. But the previously reported studies of equivalent static load design methods considered only displacement constraint conditions but not stress constraint conditions. In the present study we consider not only displacement constraint but also stress constraint conditions. Through a few numerical examples, the efficiency and reliability of proposed scheme is verified by comparison of the equivalent stress between equivalent static loading and dynamic loading.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.30 no.3A
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• pp.193-200
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• 2010

Structural design requires simultaneously to ensure safety by considering quantitatively uncertainties in the applied loadings, material properties and fabrication error and to maximize economical efficiency. As a solution, system reliability-based design optimization (SRBDO), which takes into consideration both uncertainties and economical efficiency, has been extensively researched and numerous attempts have been done to apply it to structural design. Contrary to conventional deterministic optimization, SRBDO involves the evaluation of component and system probabilistic constraints. However, because of the complicated algorithm for calculating component reliability indices and system reliability, excessive computational time is required when the large-scale finite element analysis is involved in evaluating the probabilistic constraints. Accordingly, an algorithm for SRBDO exhibiting improved stability and efficiency needs to be developed for the large-scale problems. In this study, a more stable and efficient SRBDO based on the performance measure approach (PMA) is developed. PMA shows good performance when it is applied to reliability-based design optimization (RBDO) which has only component probabilistic constraints. However, PMA could not be applied to SRBDO because PMA only calculates the probabilistic performance measure for limit state functions and does not evaluate the reliability indices. In order to overcome these difficulties, the decoupled algorithm is proposed where RBDO based on PMA is sequentially performed with updated target component reliability indices until the calculated system reliability index approaches the target system reliability index. Through a mathematical problem and ten-bar truss problem, the proposed method shows better convergence and efficiency than other approaches.

• Journal of Auto-vehicle Safety Association
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• v.7 no.3
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• pp.7-13
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• 2015

Occupant protection performance in frontal crashes has been developed and assessed for mainly front seat occupants over many years, and in recent years protection of rear seat occupants has also been extensively discussed. Unlike the front seats, the rear seats are often occupied by children seated in rear-facing or forward - facing child restraint systems, or booster seats. In the ENCAP, child occupant protection assessments using 18-month-old(P1.5) and 3-year-old(P3) test dummies in the rear seat have already been changed to new type of 18-month-old (Q1.5)and 3-year-old(Q3) test dummies. In addition, ENCAP are scheduled with the development and introduction of test dummies of 6-year-old (Q6) and 10.5-year-old children(Q10) starting 2016. In KNCAP, Q6 and Q10 child dummies will be introduced in 2017 as well. Automobile manufacturers need to develop safety performance for new child dummies closely. In this paper, we focused on Q6 and Q10 child dummies sitting in child restraint system. Offset frontal crash tests were conducted using two types of test dummies, Q6 and Q10 child dummies, positioned in the rear seat. Q6 and Q10 were used to compare dummy kinematics in rear seating positions between Q6 behind the driver's seat and Q10 behind the front passenger's seat. The full vehicle sled test results of both dummies were conducted with different restraint systems. It showed that several injury and image data was collected as the result of the full vehicle sled test. Based on the results of these investigations, this paper describes which factor is most important and combination is the best performance when evaluating rear seat occupant protection for Q6 and Q10 child dummies.